ANKA, advanced Medium Altitude Long Endurance (MALE) class Unmanned Aerial System, performs day and night, all-weather reconnaissance, target. The Anka is an advanced Medium Altitude Long Endurance (MALE) UAV ( Unmanned Aerial System) developed by the Turkish Aerospace. Turkish Aerospace has secured a new, unit order for its Anka medium-altitude , long-endurance unmanned air vehicle from the nation’s.
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The CMXD weighs in at I agree More Information. Outwardly, the Anka follows conventional UAV design and basic aircraft fundamentals to achieve a modern, sleek look.
Archived from the original on 17 May Archived from the original on 17 January The Block-B can operate at a distance of up to naka with line-of-sight LoS communications. In TIES, valuable intelligence information can be obtained by the analysis of bulky imagery data.
Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities. See the bottom of the cited webpage. The Anka sports a wingspan of over The airframe crashed, however, while attempting to land on 3 December due to a technical failure.
Archived from the original on 20 July All photos uuav author. The Anka is expected to formally enter operational service in assuming testing clears the machine for such. There is another fuselage bulge at amidships under the fuselage though this appears to be an ank fitting.
Satellite-controlled Anka-S UAV fires guided munitions
The whole composite airframe is composed of ankw monoblock fuselage, detachable wing and V-Tail, retractable landing gear, redundant control surfaces, avionics and payload bays and service doors. The system can take-off and land autonomously and personnel based at the ground control station manage the other functions as required. ANKA can be readied for flight by just three personnel in 45 minutes. An air traffic radio is also integrated in the communication system for the integration of the aircraft into the civilian airspace.
First deliveries are naka for to the Turkish Air Force for trials. Archived from the original on 14 January The S-model improves flying distances and operating altitudes over the original Anka-A systems. Within the framework of the program, a total of three prototypes and ground systems will be designed, developed, manufactured, and tested by mid as part of the prototype development phase.
TAI Anka – Wikipedia
Serial numbers and deployed on 25 March carried out more than sorties within a six month period, though the first of them experienced a crash landing on 9 October 9 the same year.
A pre-programmed mission plan can be loaded before the flight begins or can be altered during the flight. This arrangement uaav the base Anka Anka-A with a top speed of miles per hour cruise of mphan combat radius of miles with a mission endurance time of 24 hours.
Retrieved 5 January Having achieved its maiden flight in Septemberthe first ANKA-S uaf consists of two air vehicles, FLIR payloads, a satellite communications satcom capability and related ground systems. The aircraft was handed over to the Turkish Air Force in leading to production and formal introduction into service scheduled for The UAV is only part of the complete package which includes the amka itself, the ground control station, the personnel and applicable system receivers.
Retrieved from ” https: Armed with a 3kg warhead, able to penetrate mm of armour, the CIRIT can be fired either from a Smart Launcher designed by Roketsan or from a standard pod, uuav twin or quad launcher configuration.
Iav Read Edit View history. The turbocharged engine is fitted aft and powers a three-bladed propeller in a “pusher” configuration. TIES operators can initiate intelligence missions prior to or during flight.
With a service ceiling of The vehicle is powered by a single German-developed Thielert Centurion 2.
TAI Anka Unmanned Aerial Vehicle (UAV) / Unmanned Air Combat Vehicle (UCAV) – Turkey
Associated Press of Pakistan. The accepted aircraft in Blok-B configuration features a winglet due to the requirement of an additional kg in payload and 24 hours of endurance. Each Ankq Launcher weighs some 55kg in a 2-cell configuration and kg in a 4-cell, both figures including the munition. Graph average of Archived from the original on 18 November Payload volume for all is l, and payload capacity kilogrammes.
The undercarriage is a tricycle design with two main landing gear legs and a nose leg. Retrieved 23 May